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Joe D. Hoffman

Observed names: Hoffman, Joe D, Hoffman, Joe D., Hoffman,Joe D., JOE D. HOFFMAN, JOE HOFFMAN, Joe D Hoffman, Joe Hoffman
Observed institution: Purdue University West Lafayette
OpenAlex ID: A5108398247
Numerical methods for engineers and scientists
1992 · Hoffman, Joe D. · Choice Reviews Online · 1,182
Numerical Methods for Engineers and Scientists
2018 · Joe D. Hoffman, Joe D. Hoffman, et al. · CRC Press eBooks · 426
Relationship between the truncation errors of centered finite-difference approximations on uniform and nonuniform meshes
1982 · Joe D Hoffman · Journal of Computational Physics · 63
Design of compressed truncated perfect nozzles
1987 · Joe D. Hoffman · Journal of Propulsion and Power · 51
An analytical and experimental investigation of swirling flow in nozzles
1969 · DAVID J. NORTON, B. W. FARQUHAR, et al. · AIAA Journal · 27
Design of Maximum Thrust Nozzle Contours by Direct Optimization Methods
1981 · Jeffrey G. Allman, Joe D. Hoffman · AIAA Journal · 26
A Second-Order Bicharacteristics Method for Three-Dimensional, Steady, Supersonic Flow
1972 · VICTOR H. RANSOM, JOE D. HOFFMAN, et al. · AIAA Journal · 24
Calculation of three-dimensional flowfields by the unsteady method of characteristics
1985 · David L. Marcum, Joe D. Hoffman · AIAA Journal · 23
The cell Reynolds number myth
1985 · H. Doyle Thompson, Brent W. Webb, et al. · International Journal for Numerical Methods in Fluids · 19
Performance analysis of scarfed nozzles
1986 · Jay S. Lilley, Joe D. Hoffman · Journal of Spacecraft and Rockets · 18
Design of maximum thrust plug nozzles with variable inlet geometry
1974 · Gearold R. Johnson, H.Doyle Thompson, et al. · Computers & Fluids · 17
A general method for determining optimum thrust nozzle contours for chemically reacting gas flows.
1967 · JOE D. HOFFMAN · AIAA Journal · 16
Design of Shrouded-Plug Nozzles for Maximum Thrust
1974 · RICHARD VANDER VEEN, ROY GENTRY, et al. · AIAA Journal · 15
The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
1994 · Kenneth Kacynski, Joe Hoffman · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 14
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Numerical boundary condition procedures for Euler solvers
1987 · David L. Marcum, Joe D. Hoffman · AIAA Journal · 14
Accuracy studies of the numerical method of characteristics for axisymmetric, steady supersonic flows
1973 · Joe D Hoffman · Journal of Computational Physics · 13
An analytical and experimental investigation of annular propulsive nozzles
1985 · Ralph R. Conley, Joe D. Hoffman, et al. · Journal of Aircraft · 12
Optimum thrust-nozzle contours for gas-particle flows.
1967 · JOE D. HOFFMAN, H. DOYLE THOMPSON · AIAA Journal · 12
Calculation of three-dimensional inviscid flowfields in propulsive nozzles with centerbodies
1988 · David L. Marcum, Joe D. Hoffman · Journal of Propulsion and Power · 11
An analytical investigation of swirl in annular propulsive nozzles
1986 · Barbara T. Kornblum, H. Doyle Thompson, et al. · Journal of Propulsion and Power · 11
Analytical study of swirler effects in annular propulsive nozzles
1987 · Joe D. Hoffman, H. Doyle Thompson, et al. · Journal of Propulsion and Power · 10
Flow Computations in Inlets at Incidence Using a Shock Fitting Bicharacteristic Method
1980 · Joseph Vadyak, Joe D. Hoffman, et al. · AIAA Journal · 10
Comparison of Characteristic Schemes for Three-Dimensional, Steady, Isentropic Flow
1972 · MICHAEL C. CLINE, JOE D. HOFFMAN · AIAA Journal · 10
Maximum Thrust Nozzles for Nonequilibrium Simple Dissociating Gas Flows
1971 · M. PETER SCOFIELD, JOE D. HOFFMAN · AIAA Journal · 10
Three-dimensional flow simulations for supersonic mixed-compression inlets at incidence
1984 · Joseph Vadyak, Joe D. Hoffman, et al. · AIAA Journal · 9
Works count: 59
Citation count: 2,520
H-index: 14
I10-index: 25
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